View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00116U 61015A 23028.48048301 .00000029 00000-0 81320-4 0 9993
2 00116 66.8102 33.4069 0070006 56.5366 304.2380 13.91873468124706
| Epoch (UTC): | 28 January 2023 11:31:53 |
| Eccentricity: | 0.0070006 |
| inclination: | 66.8102° |
| perigee height: | 871 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 33.4069° |
| argument of perigee: | 56.5366° |
| revolutions per day: | 13.91873468 |
| mean anomaly at epoch: | 304.2380° |
| orbit number at epoch: | 12470 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|